1. 2Graves, Ernald B., and Fournier, Roger H. "Effect of Nose Bluntness and Afterbody Shape on Aerodynamic Characteristics of a Monoplanar Missile Concept With Bodies of Circular and Elliptical Cross Sections at a Mach Number of 2.50," NASA TM-80055,1979.
2. Supersonic Aerodynamic Trade Data for a Monoplanar Missile Concept
3. 4Allen, Jerry M., Hernandez, Gloria, and Lamb, Milton, "Body-Surface Pressure Data on Two Monoplane-Wing Missile Configurations WithElliptical Cross Sections atMach2.50."NASA TM-85645,1983.